View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 22236U 92080A 25199.19908323 .00001417 00000-0 12727-3 0 9990
2 22236 82.5060 143.4276 0012827 259.5112 100.4664 14.94972564766797
| Epoch (UTC): | 18 July 2025 04:46:40 |
| Eccentricity: | 0.0012827 |
| inclination: | 82.5060° |
| perigee height: | 573 km |
| apogee height: | 591 km |
| right ascension of ascending node: | 143.4276° |
| argument of perigee: | 259.5112° |
| revolutions per day: | 14.94972564 |
| mean anomaly at epoch: | 100.4664° |
| orbit number at epoch: | 76679 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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